Page History

Timeline:

• 1st meeting points:

• How many avionics towers, what does the deployment look like (probably won't be decided) *Assigned

• Approximate dimensioning, looking into what the mass would be for these systems assuming Phoenix Avionics systems weights and lengths *Assigned

  • Sustainer:

    • Weight:

    • Length:

  • Booster

    • Weight:

    • Length:

• *Need an estimate of board size from avionics

• Issue of the bay turning on in transit:

  • Did the vibration of the system cause the screw to move? If so, we may need better screw switches. This one was highly reviewed by rocketry forum: https://www.csrocketry.com/electronics/missleworks.html

  • *I need someone to come up with the test and give me commercial vibrational testers

• Incorporating a window for easy access
• *Calculations for bay sizing
• packing volume of the lines and prevent potential line entanglement issues.

• Mathinline
  body L=\frac{4V}{\pi D^{2}}

   
• 𝐿=4𝑉/𝜋𝐷^2

• LaTeX Math Block
  anchor V = \frac{w_{parachute}}{\rho_{packing}}
  V = \frac{w_{parachute}}{\rho_{packing}}

  
  

• 𝑉=𝑃𝑎𝑟𝑎𝑐ℎ𝑢𝑡𝑒 𝑤𝑒𝑖𝑔ℎ𝑡/𝑃𝑎𝑐𝑘𝑖𝑛𝑔 𝑑𝑒𝑛𝑠𝑖𝑡𝑦